COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters
AD/BELL 206/1 Fuel Booster Pump Wiring - Modification 11/67
Applicability: All model 206A with S/Nos. 4 to 20, 22 to 48, 50 to 56 59, 61 and 63. Document: Bell SL No. 206A - No. 21 Rev. A.
Compliance: Before 1 September 1971.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, form a comprehensive set of rules governing all aspects of civil aviation within Australia. Among its various parts, Part 39 specifically addresses airworthiness directives to ensure the safe operation of aircraft. One such directive, AD/BELL 206/1, targets the fuel booster pump wiring in Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters, specifically model 206A with serial numbers ranging from 4 to 20, 22 to 48, 50 to 56, 59, 61, and 63. This directive was introduced to address potential safety risks associated with the fuel booster pump wiring, aiming to ensure compliance before 1 September 1971. The policy objective behind this regulation is to enhance the overall safety of civil aviation by mitigating risks linked to specific mechanical components in certain helicopter models.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, including AD/BELL 206/1, which pertains to Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters. This directive applies to all model 206A helicopters with serial numbers within the specified ranges: 4 to 20, 22 to 48, 50 to 56, 59, 61, and 63. Compliance with this directive is mandatory for these aircraft, necessitating a modification to the fuel booster pump wiring as outlined in Bell SL No. 206A - No. 21 Rev. A, prior to 1 September 1971. The directive ensures adherence to safety standards and operational protocols by enforcing specific technical modifications, thereby maintaining airworthiness and safety in civil aviation. This regulation is applicable within the Commonwealth of Australia, governing entities and individuals operating these specific model helicopters.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39, specifically in Section 105, detail the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives (AD). In this context, AD/BELL 206/1 focuses on the fuel booster pump wiring modification for Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters. This directive applies to all model 206A helicopters with specific serial numbers ranging from 4 to 20, 22 to 48, 50 to 56, 59, 61, and 63. Compliance with this directive is required before 1 September 1971, as specified in Bell SL No. 206A - No. 21 Rev. A.
Operators and owners of the specified Bell 206A helicopters must ensure that the modifications to the fuel booster pump wiring are completed as per the directives outlined in the AD. This involves following the detailed technical instructions provided in the referenced document, Bell SL No. 206A - No. 21 Rev. A. The modifications are essential to maintain the airworthiness of the helicopters and to comply with safety standards set by CASA.
Failure to comply with AD/BELL 206/1 may result in significant legal and safety consequences. Operators and owners who do not adhere to the specified modifications may face penalties and enforcement actions by CASA. The regulations underscore the importance of timely compliance to prevent potential safety hazards, which could lead to severe accidents or operational failures. The potential penalties for non-compliance could include fines, operational restrictions, or even grounding of the affected aircraft until the necessary modifications are completed and verified.
Under the Civil Aviation Regulations 1998, the consequences for non-compliance with airworthiness directives are stringent. Operators may face civil penalties, including financial penalties and legal actions that could affect their operational licenses. Additionally, CASA has the authority to take enforcement measures, such as imposing fines, requiring corrective actions, or even prohibiting the aircraft from flying until the required modifications are verified. These measures are intended to ensure that all aircraft meet the necessary safety standards to protect passengers, crew, and the general public.